Airbus France
456Patents
226Active
456Granted
51Portfolio score
Filing activity: May 7, 2001 → Sep 23, 2009 · 226 expiring within 5 years
Most-cited patents
| Patent | Title | Area | Cited by | Status |
|---|---|---|---|---|
| US6625982B2 | Electronically controlled hydraulic actuating system | Mechanical Engineering; Lighting; Heating | 51 | Expired |
| US6536556B2 | Noise reduction sandwich panel, notably for aircraft turbojet engine | Emerging Cross-Sectional Technologies | 49 | Expired |
| US7905449B2 | Multi-engine aircraft | Emerging Cross-Sectional Technologies | 49 | Expired |
| US6827314B2 | Aircraft with active control of the warping of its wings | Emerging Cross-Sectional Technologies | 46 | Expired |
| US7926261B2 | Turbofan provided with a pre-cooler | Emerging Cross-Sectional Technologies | 44 | Active |
| US6697718B2 | Device for monitoring a plurality of systems of an aircraft, in particular of a transport aircraft | Physics | 42 | Expired |
| US7819358B2 | Aircraft with reduced environmental impact | Performing Operations; Transporting | 42 | Active |
| US6698691B2 | Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the same | Performing Operations; Transporting | 41 | Expired |
| US6708711B2 | Air inlet for commercial aircraft jet engine nacelle | Emerging Cross-Sectional Technologies | 41 | Expired |
| US6772857B2 | Acoustically resistive layer for an acoustical attenuation panel, panel using such a layer | Emerging Cross-Sectional Technologies | 41 | Expired |
| US6704624B2 | Method and device for controlling an aircraft maneuvering components, with electrical standby modules | Physics | 40 | Expired |
| US6755280B2 | Method for producing a panel comprising an adapted acoustically resistive layer and panel so obtained | Emerging Cross-Sectional Technologies | 38 | Expired |
| US6840349B2 | Multi-component acoustically resistive layer for acoustical attenuation panel and panel thus obtained | Physics | 37 | Expired |
| US6981676B2 | Method and spoiler system for ensuring the aerodynamic continuity of the upper surface of an aircraft | Performing Operations; Transporting | 36 | Expired |
| US6668215B2 | Aircraft dialog device, through which a dialog with a system of said aircraft is possible | Physics | 34 | Expired |
| US6761245B2 | Tubular acoustic attenuation piece for an aircraft jet engine air intake | Emerging Cross-Sectional Technologies | 33 | Expired |
| US6729583B2 | Device for articulating a flap to an aircraft aerodynamic surface | Emerging Cross-Sectional Technologies | 33 | Expired |
| US6443395B1 | Air inlet cowl for a jet engine equipped with de-icing means | Performing Operations; Transporting | 30 | Expired |
| US6994300B2 | Device for fastening elongate objects onto a flat support | Electricity | 30 | Expired |
| US6834834B2 | Articulation device for an aircraft door panel and an aircraft door integrating such a device | Fixed Constructions | 30 | Expired |
| US7484592B2 | Sound attenuation panel comprising a resistive layer with reinforced structural component | Physics | 28 | Expired |
| US6615950B2 | Sandwich acoustic panel | Physics | 27 | Expired |
| US6927782B2 | Airport display device | Physics | 27 | Expired |
| US6896099B2 | Aircraft engine pod with acoustic attenuation | Emerging Cross-Sectional Technologies | 26 | Expired |
| US7568659B2 | Door which is intended to be positioned between the cockpit and the cabin of an aircraft | Performing Operations; Transporting | 26 | Expired |
Source: USPTO / EPO open patent data. Counts and citation impact are objective bibliographic measures.